View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 39010U 12065C 22138.23734926 .00003023 00000-0 60651-3 0 9998
2 39010 49.6626 209.5656 4650423 324.4081 12.0694 6.18326144210939
| Epoch (UTC): | 18 May 2022 05:41:46 |
| Eccentricity: | 0.4650423 |
| inclination: | 49.6626° |
| perigee height: | 329 km |
| apogee height: | 11991 km |
| right ascension of ascending node: | 209.5656° |
| argument of perigee: | 324.4081° |
| revolutions per day: | 6.18326144 |
| mean anomaly at epoch: | 12.0694° |
| orbit number at epoch: | 21093 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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